Deposition processes for tungsten-containing barrier layers

ABSTRACT

In one embodiment, a method for forming a barrier material on a substrate is provided which includes exposing a dielectric layer on the substrate to a plasma during a preclean process, wherein the dielectric layer contains a feature having sidewalls and a bottom surface, and depositing a tungsten-containing barrier material containing tungsten nitride on the sidewalls and the bottom surface of the feature during a cyclic layer deposition process. The method further provides depositing a metal-containing seed layer on the tungsten-containing barrier material and depositing a metal-containing layer over the metal-containing seed layer to fill the feature. In another embodiment, the method provides conducting the cyclic layer deposition process within a process chamber having an expanding channel centralized above a substrate support and having a bottom surface sized and shaped to substantially cover the substrate, and sequentially exposing the substrate to precursor gases flowing from the expanding channel during the cyclic layer deposition process.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. Ser. No. 10/741,824 (APPM/7532), filed Dec. 19, 2003, and issued as U.S. Pat. No. 7,262,133, which claims benefit of U.S. Ser. No. 60/438,479 (APPM/7532L), filed Jan. 7, 2003, which are herein incorporated by reference in their entirety.

BACKGROUND OF THE INVENTION

1. Field of the Invention

Embodiments of the present invention relate to a method for manufacturing integrated circuit devices. More particularly, embodiments of the invention relate to forming thin barrier layers using cyclic or atomic layer deposition.

2. Description of the Related Art

Copper has recently become a choice metal for filling sub-micron high aspect ratio interconnect features because copper and its alloys have lower resistivities than aluminum. However, copper and its alloys have a propensity to diffuse into surrounding materials such as silicon oxide, silicon, and other dielectric materials, for example, causing an increase in the contact resistance of the circuit. Copper and its alloys also have a propensity to diffuse into surrounding elements such as transistor gates, capacitor dielectrics, transistor wells, transistor channels, electrical barrier regions, interconnects, among other known elements of integrated circuits.

FIG. 1 is a cross-sectional view of a substrate 100 including an etch stop 112 over a copper interconnect 120 in a dielectric layer 110. A barrier layer 114 is deposited prior to the deposition of copper in the interconnect to prevent or impede the diffusion of copper atoms into the surrounding dielectric layer. However, copper may still diffuse into areas surrounding the interconnect, as conventional etch stop materials, such as SiN or SiCN, do not adhere well to copper. The weak connection between the etch stop and the interconnect can result in the diffusion of metal atoms into other areas of the substrate, causing cross-talk among the interconnects of the substrate and failure of the device formed by the substrate.

There is a need, therefore, for a method for depositing an adhesive layer on metal interconnects that prevents or minimizes the diffusion of metal atoms from the interconnect.

SUMMARY OF THE INVENTION

A method for depositing a cap layer over a metal-containing interconnect by a cyclical deposition process is provided. The cap layer is formed by introducing a pulse of a metal-containing compound followed by a pulse of a nitrogen-containing compound. The cap layer provides excellent barrier properties and adheres well to the metal-containing interconnect on which it is deposited. In one aspect, the metal-containing interconnect contains copper or copper alloys, and the cap layer contains tantalum nitride.

BRIEF DESCRIPTION OF THE DRAWINGS

So that the manner in which the above recited features of the present invention are attained and can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to the embodiments thereof which are illustrated in the appended drawings.

It is to be noted, however, that the appended drawings illustrate only typical embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.

FIG. 1 illustrates a schematic, cross-sectional view of a prior art substrate.

FIG. 2 illustrates a schematic, cross-sectional view of an exemplary processing chamber 200 for use in a method of forming a cap layer according to embodiments.

FIGS. 3A-3E are cross-sectional views of a substrate illustrating steps in an embodiment of a method for forming a cap layer deposited in accordance with embodiments of a cyclical deposition technique described herein.

FIGS. 4A-4I are cross-sectional views of a substrate illustrating steps in an embodiment of a dual damascene deposition sequence.

DETAILED DESCRIPTION

Embodiments of the present invention generally provide a method of forming an adhesive cap layer on metal-containing interconnects and on a dielectric layer surrounding the metal-containing interconnects. In one embodiment, a cyclical deposition process is used to form a cap layer that is a refractory metal nitride layer having a thickness less than about 50 angstroms (Å), such as less than about 20 Å, such as from about 5 Å to about 20 Å. In one aspect of this embodiment, the refractory metal nitride layer is a tantalum nitride (TaN) layer that is preferably about 10 Å thick. In another embodiment, a cyclical deposition process is used to form a cap layer having a thickness that is sufficient to block diffusion of metal atoms from the underlying metal-containing interconnect.

The cap layers deposited according to the cyclical deposition techniques described herein provide excellent barrier properties. It is believed that the thin cap layers do not significantly change the dielectric constant of a device in which they are included.

The cap layers deposited according to the cyclical deposition methods described herein show evidence of an epitaxial growth phenomenon. In other words, the cap layers take on the same or substantially the same crystallographic characteristics as the underlying layer. For example, the cap layer over the metal-containing interconnect of the substrate has an ordered structure similar to the structure of the metal-containing interconnect, while the cap layer over the dielectric layer of the substrate has an amorphous structure similar to the amorphous structure of the dielectric layer. As a result, the cap layer adheres well to the metal-containing interconnect and enhances the reliability of the interconnect. The cap layer is amorphous and insulating over the dielectric layer and is thin enough that it is not expected to raise the effective dielectric constant of the dielectric layer.

A TaN cap layer is deposited by providing one or more pulses of a tantalum-containing compound at a flow rate between about 100 sccm and about 1,000 sccm for a time period of about 1.0 second or less and one or more pulses of a nitrogen-containing compound at a flow rate between about 100 sccm and about 1,000 sccm for a time period of about 1.0 second or less to a reaction zone having a substrate disposed therein. Exemplary tantalum-containing compounds include pentakis(ethylmethylamino) tantalum (PEMAT), pentakis(diethylamino) tantalum (PDEAT), pentakis(dimethylamino) tantalum (PDMAT) and any derivatives of PEMAT, PDEAT, and PDMAT. Exemplary tantalum-containing compounds also include t-butylimino tris(diethylamino) tantalum (TBTDET), t-butylimino tris(dimethylamino) tantalum (TBTDMT), bis(cyclopentadienyl) tantalum trihydride, bis(methylcyclopentadienyl) tantalum trihydride, and tantalum halides, such as TaX₅, where X is fluorine (F), bromine (Br), chlorine (Cl), and/or derivatives thereof. Exemplary nitrogen-containing compounds include nitrogen gas, ammonia, hydrazine, methylhydrazine, dimethlyhydrazine, t-butylhydrazine, phenylhydrazine, azoisobutane, ethylazide, and derivatives thereof.

It is to be understood that these compounds or any other compound not listed above may be a solid, liquid, or gas at room temperature. For example, PDMAT is a solid at room temperature and TBTDET is a liquid at room temperature. Accordingly, the non-gas phase precursors are subjected to a sublimation or vaporization step, which are both well known in the art, prior to introduction into the processing chamber. A carrier gas, such as argon, helium, nitrogen, hydrogen, or a mixture thereof, may also be used to help deliver the compound into the processing chamber, as is commonly known in the art.

Each pulse is performed sequentially, and is accompanied by a separate flow of non-reactive gas at a rate between about 200 sccm and about 1,000 sccm. The separate flow of non-reactive gas may be pulsed between each pulse of the reactive compounds or the separate flow of non-reactive gas may be introduced continuously throughout the deposition process. The separate flow of non-reactive gas, whether pulsed or continuous, serves to remove any excess reactants from the reaction zone to prevent unwanted gas phase reactions of the reactive compounds, and also serves to remove any reaction by-products from the processing chamber, similar to a purge gas. In addition to these services, the continuous separate flow of non-reactive gas helps deliver the pulses of reactive compounds to the substrate surface similar to a carrier gas. The term “non-reactive gas” as used herein refers to a single gas or a mixture of gases that does not participate in the metal layer formation. Exemplary non-reactive gases include argon, helium, nitrogen, hydrogen, and combinations thereof.

A “compound” is intended to include one or more precursors, reductants, reactants, and catalysts. Each compound may be a single compound or a mixture/combination of two or more compounds.

A “thin layer” as used herein refers to a layer of material deposited on a substrate surface having a thickness of about 20 Å or less, such as about 10 Å. A “feature” as used herein refers to a via, contact, line, or any other interconnect facet, e.g., vertical or horizontal interconnect, having an aspect ratio (height to width ratio) of about 4:1 or greater. A “substrate surface”, as used herein, refers to any substrate surface upon which film processing is performed. For example, a substrate surface may include silicon, silicon oxide, doped silicon, germanium, gallium arsenide, glass, sapphire, and any other materials such as metals, metal alloys, and other conductive materials, depending on the application. A substrate surface may also include dielectric materials such as silicon dioxide and carbon doped silicon oxides.

“Cyclical deposition” as used herein refers to the sequential introduction of two or more compounds to deposit a thin layer on a substrate surface. The two or more compounds are sequentially introduced into a reaction zone of a processing chamber. Each compound is separated by a time delay/pause to allow each compound to adhere and/or react on the substrate surface. In one aspect, a first compound or compound A is dosed/pulsed into the reaction zone followed by a first time delay/pause. Next, a second compound or compound B is dosed/pulsed into the reaction zone followed by a second time delay. When a ternary material is desired, a third compound (C), is dosed/pulsed into the reaction zone followed by a third time delay. These sequential tandems of a pulse of reactive compound followed by a time delay may be repeated indefinitely until a desired film or film thickness is formed on the substrate surface.

A “pulse/dose” as used herein is intended to refer to a quantity of a particular compound that is intermittently or non-continuously introduced into a reaction zone of a processing chamber. The quantity of a particular compound within each pulse may vary over time, depending on the duration of the pulse. A particular compound may include a single compound or a mixture/combination of two or more compounds.

A “reaction zone” is intended to include any volume that is in fluid communication with a substrate surface being processed. The reaction zone may include any volume within a processing chamber that is between a gas source and the substrate surface. For example, the reaction zone includes any volume downstream of a dosing valve in which a substrate is disposed.

The durations for each pulse/dose are variable and may be adjusted to accommodate, for example, the volume capacity of the processing chamber as well as the capabilities of a vacuum system coupled thereto. Additionally, the dose time of a compound may vary according to the flow rate of the compound, the pressure of the compound, the temperature of the compound, the type of dosing valve, the type of control system employed, as well as the ability of the compound to adsorb onto the substrate surface. Dose times may also vary based upon the type of layer being formed and the geometry of the device being formed.

Typically, the duration for each pulse/dose or “dose time” is about 1.0 second or less. However, a dose time can range from microseconds to milliseconds to seconds, and even to minutes. In general, a dose time should be long enough to provide a volume of compound sufficient to adsorb/chemisorb onto substantially the entire surface of the substrate and form a layer of the compound thereon.

FIG. 2 illustrates a schematic, partial cross section of an exemplary processing chamber 200 for use in a method of forming a barrier layer according to each of the embodiments of the present invention. Such a processing chamber 200 is available from Applied Materials, Inc. located in Santa Clara, Calif., and a brief description thereof follows. A more detailed description may be found in commonly assigned U.S. Ser. No. 10/032,284, filed on Dec. 21, 2001, and issued as U.S. Pat. No. 6,916,398, which is incorporated herein by reference.

The processing chamber 200 may be integrated into an integrated processing platform, such as an ENDURA® platform also available from Applied Materials, Inc. Details of the ENDURA® platform are described in commonly assigned U.S. Ser. No. 09/451,628, entitled “Integrated Modular Processing Platform,” filed on Nov. 30, 1999, which is incorporated by reference herein.

The chamber 200 includes a chamber body 202 having a slit valve 208 formed in a sidewall 204 thereof and a substrate support 212 disposed therein. The substrate support 212 is mounted to a lift motor 214 disposed through the bottom 206 of the chamber body 202 to raise and lower the substrate support 212 and a substrate 210 disposed on an upper surface 211 of the substrate support 212. The substrate support 212 may also include a vacuum chuck, an electrostatic chuck, or a clamp ring for securing the substrate 210 to the substrate support 212 during processing. Further, the substrate support 212 may be heated using an embedded heating element, such as a resistive heater, or may be heated using radiant heat, such as heating lamps disposed above the substrate support 212. A purge ring 222 may be disposed on the substrate support 212 to define a purge channel 224 that provides a purge gas to prevent deposition on a peripheral portion of the substrate 210.

A gas delivery apparatus 230 is disposed at an upper portion of the chamber body 202 to provide a gas, such as a process gas and/or a purge gas, to the chamber 200. A vacuum system 278 is in communication with a pumping channel 279 to evacuate gases from the chamber 200 and to help maintain a desired pressure or a desired pressure range inside a pumping zone 266 of the chamber 200.

The gas delivery apparatus 230 includes a chamber lid 232 having an expanding channel 264 formed within a central portion thereof. The chamber lid 232 also includes a bottom surface 260 extending from the expanding channel 264 to a peripheral portion of the chamber lid 232. The bottom surface 260 is sized and shaped to substantially cover the substrate 210 disposed on the substrate support 212. The expanding channel 264 has an inner diameter that gradually increases from an upper portion 237 to a lower portion 235 adjacent the bottom surface 260 of the chamber lid 232. The velocity of a gas flowing therethrough decreases as the gas flows through the expanding channel 264 due to the expansion of the gas. The decreased gas velocity reduces the likelihood of blowing off reactants adsorbed on the surface of the substrate 210.

Although the exact flow pattern of the gases that flow through the expanding channel 264 is not known, it is believed that the gases may travel with a circular flow pattern, such as a vortex, a helix, a spiral, or derivatives thereof, through the expanding channel 264. The circular flow or vortex flow may be provided in a processing region as opposed to in a compartment separated from the substrate 210. In one aspect, the vortex flow may help to establish a more efficient purge of the expanding channel 264 due to the sweeping action of the vortex flow pattern across the inner surface of the expanding channel 264.

In one embodiment, the distance between the gas inlets and the substrate 210 is made long enough that the vortex flow dissipates downwardly as a spiral flow across the surface of the substrate 210. It is believed that the vortex flow proceeds in a laminar manner efficiently purging the surface of the chamber lid 232 and the substrate 210. In one specific embodiment the distance between the upper portion 237 of the expanding channel 264 and the substrate 210 is about 1.0 inch or more, more preferably about 2.0 inches or more. In one specific embodiment, the upper limit of the distance is dictated by practical limitations. For example, if the distance is very long, then the residence time of a gas traveling though the expanding channel 264 would be long, then the time for a gas to deposit onto the substrate would be long, and then throughput would be low. In addition, if the distance is very long, manufacturing of the expanding channel 264 would be difficult. In general, the upper limit of distance may be 3 inches or more for a chamber adapted to process 200 mm diameter substrates or 5 inches or more for a chamber adapted to process 300 mm diameter substrates.

Referring to FIG. 2, at least a portion of the bottom surface 260 of the chamber lid 232 may be tapered from the expanding channel 264 to a peripheral portion of the chamber lid 232 to help provide an improved velocity profile of a gas flow from the expanding channel 264 across the surface of the substrate 210 (i.e., from the center of the substrate to the edge of the substrate). The bottom surface 260 may comprise one or more tapered surfaces, such as a straight surface, a concave surface, a convex surface, or combinations thereof. In one embodiment, the bottom surface 260 is tapered in the shape of a funnel.

The gas delivery apparatus 230 also includes at least two high speed actuating valves 242A, 242B having one or more ports. At least one valve 242A, 242B is dedicated to each reactive compound. For example, a first valve is dedicated to a refractory metal-containing compound, such as tantalum and a second valve is dedicated to a nitrogen-containing compound. When a ternary material is desired, a third valve is dedicated to an additional compound.

The valves 242A, 242B may generally be any type of valve capable of reliably, repeatedly, and precisely metering the desired precursors at the desired rate of introduction. In some cases, dosing may be as fast as 1-2 milliseconds (msec). As one example, the valves 242A, 242B may be electronically controlled (EC) valves, which are commercially available from Fujikin of Japan as part number FR-21-6.35 UGF-APD. The valves 242A, 242B precisely and repeatedly deliver short pulses of the reactive compounds into the chamber body 202. The valves 242A, 242B can be directly controlled by a system computer, such as a mainframe for example, or controlled by a chamber/application specific controller, such as a programmable logic computer (PLC) which is described in more detail in the co-pending U.S. Ser. No. 09/800,881, filed on Mar. 7, 2001, and issued as U.S. Pat. No. 6,734,020, which is incorporated by reference herein.

An exemplary process for forming a TaN cap layer on a 200 mm wafer using a cyclical deposition process of alternate/sequential pulses of PDMAT and ammonia is described below. The process may be performed within a processing chamber, such as the processing chamber 200 described in FIG. 1. PDMAT is a preferred tantalum-containing compound for a number of reasons. PDMAT is relatively stable, and has a vapor pressure which makes it easy to deliver. PDMAT may also be produced with a low halide content, such as less than 100 ppm, and may even be produced with a halide content of less than 30 ppm or even less than 5 ppm. Not wishing to be bound by theory, it is believed that an organo-metallic precursor with a low halide content is beneficial because halides (such as chlorine) incorporated in the cap layer may attack an adjacent copper layer.

To deposit the TaN layer, an inert/purge gas such as argon is first introduced into the processing chamber 200 to stabilize the pressure and temperature therein. This separate flow of an inert/purge gas flows continuously during the deposition process such that only the separate flow of an inert/purge gas flows between pulses of each compound. After the chamber pressure and temperature have been stabilized between about 150° C. and about 350° C. at about 0.5 Torr to about 5 Torr, a first pulse of PDMAT is provided from the gas source 238 at a flow rate between about between about 100 sccm and about 400 sccm, with a pulse time of about 0.6 seconds or less. A pulse of ammonia is then provided from the gas source 239 at a flow rate between about 200 sccm and about 600 sccm, with a pulse time of about 0.6 seconds or less.

A pause between pulses of PDMAT and ammonia is about 1.0 second or less, about 0.5 seconds or less, or about 0.1 seconds or less. A pause after the pulse of ammonia is also about 1.0 second or less, about 0.5 seconds or less, or about 0.1 seconds or less. Argon gas flowing between about 100 sccm and about 1,000 sccm, such as between about 100 sccm and about 400 sccm, is continuously provided from the gas source 240 through each valve 242A, 242B. In one aspect, at least a portion of a pulse of PDMAT may still be in the chamber when at a least a portion of a pulse of ammonia enters so that some co-reaction, e.g., a gas phase co-reaction, takes place. In another aspect, the duration of the purge gas and/or pump evacuation is designed to prevent the pulses of PDMAT and ammonia from mixing together in the reaction zone.

The heater temperature is maintained between about 150° C. and about 350° C. at a chamber pressure between about 0.5 Torr and about 5.0 Torr. Each cycle consisting of a pulse of PDMAT, pause, pulse of ammonia, and pause provides a tantalum nitride layer having a thickness between about 0.3 Å and about 1.0 Å. The alternating sequence may be repeated until the desired thickness is achieved, which is less than about 20 Å, such as about 10 Å. Accordingly, the deposition method requires between 10 cycles and 70 cycles, more typically between 20 cycles and 30 cycles.

FIGS. 3A-3E are cross sectional views of a substrate at different stages of a multi-layer metal interconnect fabrication sequence incorporating a thin cap layer deposited using a cyclical deposition process described herein. FIG. 3A shows an underlying layer 310, such as a lower level metal interconnect, of substrate 300 having a dielectric layer 312 formed thereon. The dielectric layer 312 may be any dielectric material including a low k dielectric material, whether presently known or yet to be discovered. For example, the dielectric layer 312 may be a silicon oxide or a carbon doped silicon oxide, for example. The dielectric layer 312 has been etched to form a feature 314, such as a hole, therein using conventional and well-known techniques. The feature 314 may be a plug, via, contact, line, wire, or any other interconnect component. The feature 314 has vertical sidewalls 316 and a bottom 318, typically having an aspect ratio of 4:1 or greater, such as 6:1. The bottom 318 exposes at least a portion of the underlying layer 310.

Referring to FIG. 3B, a barrier layer 330 is deposited on the bottom 318 as well as the side walls 316 of the feature 314. Preferably, the barrier layer 330 has a thickness less than about 20 Å, more preferably, a thickness of about 10 Å. The barrier layer may be deposited by CVD, PVD, a cyclical deposition process as described herein, or combinations thereof. The barrier layer may include TaN, Ta TiSiN, tungsten (W), tungsten nitride (WN_(x)) or combinations thereof, such as a layer of TaN and a layer of Ta. The barrier layer 330 prevents or minimizes diffusion of material subsequently deposited in the feature 314 into the dielectric layer 312.

Optionally, the patterned or etched substrate dielectric layer 312 may be cleaned to remove native oxides or other contaminants from the surface thereof prior to depositing the barrier layer 330. For example, reactive gases may be excited into a plasma within a remote plasma source chamber and delivered to the processing chamber 200. An exemplary remote plasma chamber is a Reactive Preclean II chamber available from Applied Materials, Inc., located in Santa Clara, Calif. Alternatively, the processing chamber 200 may be modified to deliver the pre-cleaning gas plasma through existing gas inlets.

In one aspect, the reactive pre-clean process forms radicals from a plasma of one or more reactive gases such as argon, helium, hydrogen, nitrogen, fluorine-containing compounds, and combinations thereof. For example, a reactive gas may include a mixture of tetrafluorocarbon (CF₄) and oxygen (O₂), or a mixture of helium (He) and nitrogen trifluoride (NF₃).

The plasma is typically generated by applying a power of about 500 watts to 2,000 watts RF at a frequency of about 200 KHz to 114 MHz. The flow of reactive gases ranges between about 100 sccm and about 1,000 sccm and the plasma treatment lasts for about 10 seconds to about 150 seconds. Preferably, the plasma is generated in one or more treatment cycles and purged between cycles. For example, four treatment cycles lasting 35 seconds each is effective.

In another aspect, the patterned or etched dielectric layer 312 may be pre-cleaned first using an argon plasma and then a hydrogen plasma. A processing gas having greater than about 50% argon by number of atoms is introduced at a pressure of about 0.8 mTorr. A plasma is struck to subject the dielectric layer 312 to an argon sputter cleaning environment. The argon plasma is preferably generated by applying between about 50 watts and about 500 watts of RF power. The argon plasma is maintained for between about 10 seconds and about 300 seconds to provide sufficient cleaning time for the deposits that are not readily removed by a reactive hydrogen plasma. Following the argon plasma, the chamber pressure is increased to about 140 mTorr, and a processing gas consisting essentially of hydrogen and helium is introduced into the processing region. Preferably, the processing gas comprises about 5% hydrogen and about 95% helium. The hydrogen plasma is generated by applying between about 50 watts and about 500 watts power. The hydrogen plasma is maintained for about 10 seconds to about 300 seconds.

Referring to FIG. 3C, a metal-containing seed layer 340, such as a metal, metal alloy, or a combination thereof is deposited over the barrier layer 330 to at least partially fill the feature 314. In one aspect, a metal-containing seed layer 340 of a copper-containing material is first deposited having a thickness of about 1,000 Å to about 2,000 Å before a metal-containing layer 342, such as a copper layer is deposited over the metal-containing seed layer 340 to fill the feature 314, as shown in FIG. 3D.

In one aspect, the metal-containing seed layer 340 is deposited using high density plasma physical vapor deposition (HDP-PVD) to enable good conformal coverage. One example of a HDP-PVD chamber is the Ionized Metal Plasma (IMP) chamber, such as the VECTRA IMP SOURCE® chamber, available from Applied Materials, Inc. of Santa Clara, Calif. The IMP chamber may also be integrated into an ENDURA® platform, also available from Applied Materials, Inc. Of course, other techniques, such as physical vapor deposition, chemical vapor deposition, electroless plating, and electroplating, may be used.

The IMP chamber includes a target, coil, and biased substrate support member. To form the metal-containing seed layer 340, a power between about 0.5 kW and about 5 kW is applied to the target, and a power between about 0.5 kW and 3 kW is applied to the coil. A power between about 200 watts and about 500 watts at a frequency of about 13.56 MHz is applied to bias the substrate. Argon is flowed into the chamber at a rate of about 35 sccm to about 85 sccm, and nitrogen may be added to the chamber at a rate of about 5 sccm to about 100 sccm. The substrate support member is heated to a temperature between about 50° C. and 250° C. as the pressure of the chamber is typically between about 5 mTorr to about 100 mTorr.

Referring to FIG. 3D, the metal-containing layer 342 may be deposited over the metal-containing seed layer 340 using CVD, PVD, electroless, or electroplating techniques. In one aspect, a metal-containing layer 342 of copper is formed using an electroplating cell, such as the ELECTRA® Cu ECP system, available from Applied Materials, Inc., of Santa Clara, Calif. The ELECTRA® Cu ECP system may also be integrated into an ENDURA® platform also available from Applied Materials, Inc. A copper electrolyte solution and copper electroplating technique is described in commonly assigned U.S. Pat. No. 6,113,771, which is incorporated by reference herein. Typically, the electroplating bath has a copper concentration greater than about 0.7 M. The electroplating bath may also contain various additives as is well known in the art. The temperature of the bath is between about 15° C. and about 25° C. The bias is between about −15 volts to about 15 volts. In one aspect, the positive bias ranges from about 0.1 volts to about 10 volts and the negatives bias ranges from about −0.1 volts to about −10 volts.

While FIG. 3D shows a metal-containing seed layer 340 underlying the metal-containing layer 342 that fills the feature 314, the metal-containing layer 342 may be deposited on the barrier layer 330 without an underlying seed layer by a technique such as PVD, CVD, electroplating, electroless plating, and combinations thereof.

Following the deposition of the metal-containing layer, the top portion of the resulting substrate may be planarized, as shown in FIG. 3D. A chemical mechanical planarizing (CMP) apparatus may be used, such as the MIRRA® System available from Applied Materials, Inc., located in Santa Clara, Calif., for example. For example, portions of the metal-containing seed layer 340, the metal-containing layer 342, and the dielectric layer 312 are removed from the top of the structure leaving a fully planar surface. Optionally, the intermediate surfaces of the structure may be planarized between the depositions of the subsequent layers described above.

Optionally, an anneal treatment may be performed following chemical mechanical polishing whereby the substrate is subjected to a temperature between about 100° C. and about 400° C. for about 10 minutes to about 1 hour, preferably about 30 minutes. A non-reactive gas such as helium, hydrogen, nitrogen, or a mixture thereof is introduced at a rate of 100 sccm to about 10,000 sccm. The chamber pressure is maintained between about 2 Torr and about 10 Torr. The RF power is about 200 watts to about 1,000 watts at a frequency of about 13.56 MHz, and the preferable substrate spacing is between about 300 mils and about 800 mils.

A cap layer 350 is then deposited on the substrate, as shown in FIG. 3E. The cap layer 350 is deposited by a cyclical deposition process described herein. For example, the cap layer may be a tantalum nitride layer about 10 Å thick. It is believed that the region 352 of the cap layer 350 over the metal-containing layer 342 has a structure similar to the structure of the metal-containing layer 342, while the region 354 of the cap layer 350 over the dielectric layer 312 has a structure similar to the structure of the dielectric layer 312.

In one embodiment, an etch stop layer 360, such as a SiN layer or a SiCN layer, is then deposited on the cap layer 350. The etch stop layer 360 may be deposited by PVD, CVD, other deposition techniques, or combinations thereof. Additional layers (not shown), such as dielectric layers and metal-containing layers, may be deposited on the etch stop layer 360.

A preferred method for making a dual damascene structure including the cap layer described herein is sequentially depicted in FIGS. 4A-4I, which are cross sectional views of a substrate having the steps of an embodiment performed thereon. As shown in FIG. 4A, an initial first dielectric layer 510, such as a low dielectric constant film, is deposited on a liner or barrier layer 512 to a thickness, such as between about 5,000 Å and about 10,000 Å, depending on the size of the structure to be fabricated. The liner layer 512 may be a silicon carbide layer which may be doped with oxygen or nitrogen. The liner/barrier layer 512 may alternatively comprise another material, such as silicon nitride, which minimizes the oxidation of conductive materials, such as copper, which may comprise conductive features 502 previously formed in the substrate 500.

As shown in FIG. 4B, an etch stop layer 514, which may be a silicon carbide layer or doped silicon carbide layer is then deposited on the first dielectric layer to a thickness, such as between about 200 Å and about 1,000 Å using RF power in the range between about 10 watts and about 1000 watts for a 200 mm substrate. The etch stop layer 514 is then pattern etched to define the contact/via openings 516 and to expose first dielectric layer 510 in the areas where the contacts/vias are to be formed as shown in FIG. 4C. Preferably, the etch stop layer 514 is pattern etched using conventional photolithography and etch processes.

After the etch stop layer 514 has been etched to pattern the contacts/vias 516 and the photo resist has been removed, a second dielectric layer 518 is deposited over the first etch stop layer 514 to a thickness, such as between about 5,000 Å and about 10,000 Å as described for the first dielectric layer 510 as shown in FIG. 4D.

A second etch stop layer 519, which may be a silicon carbide layer or doped silicon carbide layer is then deposited on the second dielectric layer 518 to a thickness, such as of about 200 to about 1000 Å. The silicon carbide material may be doped with oxygen or nitrogen. A photoresist 522 deposited on second etch stop layer 519 is then patterned, as shown in FIG. 4E. Line openings 520 and contacts/vias 516 are then etched using reactive ion etching or other anisotropic etching techniques to define the metallization structure (i.e., the openings for the lines and contact/via) and expose the conductive feature 502 as shown in FIG. 4F. Any photoresist 522 or other material used to pattern and etch the second etch stop layer 519 is removed using an oxygen strip or other suitable process.

Following etching of the deposited material and removal of photo resist materials, exposed portions of the second etch stop layer 519, the second dielectric layer 518, the first etch stop layer 514, the first dielectric layer 510, and the liner or barrier layer 512 may be treated with a reactive pre-clean process, as described above, to remove contaminants, particulate matter, residues, and oxides that may have formed on the exposed portions of the contact/via openings 516, the line openings 520, and the conductive feature 502.

The metallization structure is then formed with a conductive material such as aluminum, copper, tungsten or combinations thereof. Presently, the trend is to use copper to form the smaller features due to the low resistivity of copper (1.7 Ω-cm compared to 5.1 Ω-cm for aluminum). Preferably, as shown in FIG. 4G, a conductive barrier layer 524 is first deposited conformably in the metallization pattern to prevent copper migration into the surrounding silicon and/or dielectric material. Barrier layers include titanium, titanium nitride, tantalum, tantalum nitride, and combinations thereof, among other conventional barrier layer materials. Thereafter, the metal-containing layer 526 of copper is deposited using either chemical vapor deposition, physical vapor deposition, electroplating, or combinations thereof to form the conductive structure. Once the structure has been filled with copper or other metal, the surface is planarized using chemical mechanical planarizing as shown in FIG. 4H.

Optionally, the structure may be annealed after chemical mechanical polishing, as described above.

A cap layer 530 is then deposited on the structure, as shown in FIG. 4I. The cap layer 530 is deposited by a cyclical deposition process described herein. For example, the cap layer may be a tantalum nitride layer about 10 Å thick. It is believed that the region 540 of the cap layer over the metal-containing layer 526 has a structure similar to the structure of the metal-containing layer 526.

In one embodiment, an etch stop layer 532, such as a SiN layer or a SiCN layer, is then deposited on the cap layer 530, as shown in FIG. 4I. The etch stop layer 532 may be deposited by PVD, CVD, other deposition techniques, or combinations thereof. Additional layers (not shown), such as dielectric layers and metal-containing layers, may be deposited on the etch stop layer 532.

As stated above, the processing steps of the embodiments described herein may be performed in an integrated processing platform such as the ENDURA® platform available from Applied Materials, Inc. of Santa Clara, Calif. To facilitate the control and automation of the overall system, the integrated processing system may include a controller 280 comprising a central processing unit (CPU) 282, memory 284, and support circuits 286. The CPU 282 may be one of any form of computer processors that are used in industrial settings for controlling various drives and pressures. The memory 284 is connected to the CPU 282, and may be one or more of a readily available memory such as random access memory (RAM), read only memory (ROM), floppy disk, hard disk, or any other form of digital storage, local or remote. Software instructions and data can be coded and stored within the memory 284 for instructing the CPU 282. The support circuits 286 are also connected to the CPU 282 for supporting the processor 282 in a conventional manner. The support circuits 286 may include cache, power supplies, clock circuits, input/output circuitry, subsystems, and the like.

While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow. 

1. A method for forming a barrier material on a substrate, comprising: exposing a dielectric layer on a substrate to a plasma during a preclean process, wherein the dielectric layer comprises a feature having sidewalls and a bottom surface; depositing a tungsten-containing barrier material on the sidewalls and the bottom surface of the feature during a cyclic layer deposition process, wherein the tungsten-containing barrier material comprises tungsten nitride; depositing a metal-containing seed layer on the tungsten-containing barrier material; and depositing a metal-containing layer over the metal-containing seed layer to fill the feature.
 2. The method of claim 1, wherein the tungsten-containing barrier material comprises tungsten and tungsten nitride.
 3. The method of claim 1, wherein the tungsten-containing barrier material has a thickness of less than about 20 Å.
 4. The method of claim 3, wherein the thickness is about 10 Å.
 5. The method of claim 1, wherein the plasma is formed by a remote plasma system.
 6. The method of claim 5, wherein the preclean process and the cyclic layer deposition process are in the same process chamber.
 7. The method of claim 1, wherein the cyclic layer deposition process is performed within a process chamber comprising: a chamber lid; a substrate support; and an expanding channel centralized above the substrate support and having a bottom surface sized and shaped to substantially cover the substrate.
 8. The method of claim 7, wherein the substrate is sequentially exposed to precursor gases flowing from the expanding channel during the cyclic layer deposition process.
 9. The method of claim 8, wherein the precursor gases comprise a metal-containing precursor and ammonia gas.
 10. The method of claim 8, wherein the precursor gases are exposed to the substrate having a circular flow pattern selected from the group consisting of vortex, helix, spiral, and derivatives thereof.
 11. The method of claim 1, wherein the metal-containing layer is deposited by a chemical vapor deposition process.
 12. The method of claim 11, wherein the metal-containing layer comprises tungsten.
 13. The method of claim 1, wherein the metal-containing seed layer and the metal-containing layer comprise copper.
 14. A method for forming a barrier material on a substrate, comprising: positioning a substrate within a process chamber, the process chamber comprising: a chamber lid; a substrate support; and an expanding channel centralized above the substrate support and having a bottom surface sized and shaped to substantially cover the substrate; depositing a tungsten-containing barrier material on the substrate during a cyclic layer deposition process, wherein the tungsten-containing barrier material comprises tungsten nitride and the cyclic layer deposition process comprises sequentially exposing the substrate to precursor gases flowing from the expanding channel; depositing a metal-containing seed layer on the tungsten-containing barrier material; and depositing a metal-containing layer over the metal-containing seed layer.
 15. The method of claim 14, wherein the tungsten-containing barrier material comprises tungsten and tungsten nitride.
 16. The method of claim 14, wherein the tungsten-containing barrier material has a thickness of less than about 20 Å.
 17. The method of claim 16, wherein the thickness is about 10 Å.
 18. The method of claim 14, wherein the precursor gases comprise a metal-containing precursor and ammonia gas.
 19. The method of claim 14, wherein the precursor gases are exposed to the substrate having a circular flow pattern selected from the group consisting of vortex, helix, spiral, and derivatives thereof.
 20. The method of claim 19, wherein the process chamber further comprises a remote plasma system.
 21. The method of claim 20, wherein the substrate is exposed to a plasma during a preclean process prior to depositing the tungsten-containing barrier material.
 22. The method of claim 14, wherein the metal-containing layer is deposited by a chemical vapor deposition process.
 23. The method of claim 22, wherein the metal-containing layer comprises tungsten.
 24. A method for forming a barrier material on a substrate, comprising: depositing a tungsten-containing barrier material on a substrate during a cyclic layer deposition process, wherein the tungsten-containing barrier material comprises tungsten and tungsten nitride; depositing a metal-containing seed layer on the tungsten-containing barrier material; and depositing a metal-containing layer over the metal-containing seed layer during a chemical vapor deposition process.
 25. The method of claim 24, wherein the tungsten-containing barrier material has a thickness of less than about 20 Å.
 26. The method of claim 25, wherein the thickness is about 10 Å.
 27. The method of claim 24, wherein the cyclic layer deposition process is performed within a process chamber comprising: a chamber lid; a substrate support; and an expanding channel centralized above the substrate support and having a bottom surface sized and shaped to substantially cover the substrate.
 28. The method of claim 27, wherein the substrate is sequentially exposed to precursor gases flowing from the expanding channel during the cyclic layer deposition process.
 29. The method of claim 28, wherein the precursor gases comprise a metal-containing precursor and ammonia gas.
 30. The method of claim 28, wherein the precursor gases are exposed to the substrate having a circular flow pattern selected from the group consisting of vortex, helix, spiral, and derivatives thereof.
 31. The method of claim 27, wherein the process chamber further comprises a remote plasma system.
 32. The method of claim 31, wherein the substrate is exposed to a plasma during a preclean process prior to depositing the tungsten-containing barrier material.
 33. The method of claim 24, wherein the metal-containing layer comprises tungsten. 